CN1083787C - 使用高度偏心轨道和大气制动方法发射卫星的方法 - Google Patents

使用高度偏心轨道和大气制动方法发射卫星的方法 Download PDF

Info

Publication number
CN1083787C
CN1083787C CN97126276A CN97126276A CN1083787C CN 1083787 C CN1083787 C CN 1083787C CN 97126276 A CN97126276 A CN 97126276A CN 97126276 A CN97126276 A CN 97126276A CN 1083787 C CN1083787 C CN 1083787C
Authority
CN
China
Prior art keywords
orbit
star
satellite
main
track
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN97126276A
Other languages
English (en)
Chinese (zh)
Other versions
CN1195630A (zh
Inventor
克里斯托福·考贝尔
多米尼克·瓦伦蒂安
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of CN1195630A publication Critical patent/CN1195630A/zh
Application granted granted Critical
Publication of CN1083787C publication Critical patent/CN1083787C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242Orbits and trajectories
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242Orbits and trajectories
    • B64G1/2427Transfer orbits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085Swarms and constellations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/002Launch systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
CN97126276A 1996-12-31 1997-12-30 使用高度偏心轨道和大气制动方法发射卫星的方法 Expired - Fee Related CN1083787C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9616276 1996-12-31
FR9616276A FR2757825B1 (fr) 1996-12-31 1996-12-31 Procede et systeme de lancement simultane de satellites sur des orbites non coplanaires en utilisant des orbites tres excentriques et du freinage atmospherique

Publications (2)

Publication Number Publication Date
CN1195630A CN1195630A (zh) 1998-10-14
CN1083787C true CN1083787C (zh) 2002-05-01

Family

ID=9499352

Family Applications (1)

Application Number Title Priority Date Filing Date
CN97126276A Expired - Fee Related CN1083787C (zh) 1996-12-31 1997-12-30 使用高度偏心轨道和大气制动方法发射卫星的方法

Country Status (7)

Country Link
US (1) US5961077A (de)
EP (1) EP0854083B1 (de)
JP (1) JPH1179100A (de)
CN (1) CN1083787C (de)
DE (1) DE69730110T2 (de)
FR (1) FR2757825B1 (de)
RU (1) RU2220886C2 (de)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6843446B2 (en) * 1993-11-12 2005-01-18 David D. Scott Apparatus and methods for in-space satellite operations
US6257526B1 (en) * 1998-11-09 2001-07-10 Hughes Electronics Corporation Satellite system and method of deploying same
US6327523B2 (en) 1999-01-21 2001-12-04 Hughes Electronics Corporation Overhead system of inclined eccentric geosynchronous orbitting satellites
US6364252B1 (en) * 1999-03-11 2002-04-02 Constellation Services International, Inc. Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair
US20020130222A1 (en) * 1999-03-11 2002-09-19 Constellation Services International Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair
US6453220B1 (en) * 2000-01-31 2002-09-17 Space Systems/Loral, Inc. Low earth orbit satellite constellation stationkeeping algorithm with absolute altitude control
US7184761B1 (en) 2000-03-27 2007-02-27 The Directv Group, Inc. Satellite communications system
US7369809B1 (en) 2000-10-30 2008-05-06 The Directv Group, Inc. System and method for continuous broadcast service from non-geostationary orbits
US6830222B1 (en) 2002-03-21 2004-12-14 Global Aerospace Corporation Balloon device for lowering space object orbits
US7832687B1 (en) 2004-08-24 2010-11-16 Lockheed Martin Corporation On-orbit storage, plane change, and injection to final orbit of space vehicles
US7689358B2 (en) * 2006-04-25 2010-03-30 Northrop Grumman Corporation Delta-V-free satellite cloud cluster flying
FR2982045B1 (fr) * 2011-10-28 2013-12-27 Thales Sa Procede et systeme de commande d'un ensemble d'au moins deux satellites adaptes pour fournir un service
US8655589B2 (en) * 2012-01-25 2014-02-18 Mitsubishi Electric Research Laboratories, Inc. System and method for controlling motion of spacecrafts
US9114893B2 (en) * 2012-07-26 2015-08-25 Mitsubishi Electric Research Laboratories, Inc. System and method for estimating states of spacecraft in planet-moon environment
US8768622B2 (en) * 2012-09-14 2014-07-01 The United States Of America, As Represented By The Secretary Of The Navy System and method for maneuver plan for satellites flying in proximity using apocentral coordinate system
CN103072703B (zh) * 2013-01-30 2013-10-16 北京控制工程研究所 一种欠驱动的卫星进动控制方法
CN103072701B (zh) * 2013-01-30 2013-10-16 北京控制工程研究所 一种欠驱动的卫星消旋控制方法
US9284068B2 (en) * 2014-04-08 2016-03-15 The Boeing Company Fast-low energy transfer to Earth-Moon Lagrange point L2
FR3020348B1 (fr) * 2014-04-24 2016-05-13 Snecma Procede de deploiement d'une constellation de satellites
CN104354880B (zh) * 2014-10-17 2016-08-17 北京航空航天大学 一种用于空间姿态调整的双偏心盘装置
RU2583507C1 (ru) * 2015-02-05 2016-05-10 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ одновременного выведения группы спутников на некомпланарные орбиты (варианты)
US10313010B2 (en) * 2015-03-17 2019-06-04 The Boeing Company Laser communications in super-geosynchronous earth orbit
US10009101B2 (en) 2015-03-17 2018-06-26 The Boeing Company Laser communications following an atmospheric event
RU2605463C2 (ru) * 2015-04-03 2016-12-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления транспортной космической системой
US9919813B2 (en) 2015-04-15 2018-03-20 The United States Of America, As Represented By The Secretary Of The Navy Control system and method for a plane change for satellite operations
JP6542581B2 (ja) * 2015-05-19 2019-07-10 株式会社Ihiエアロスペース 宇宙機とその軌道面変更方法
RU2614466C2 (ru) * 2015-07-20 2017-03-28 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления транспортной космической системой
RU2643082C1 (ru) * 2016-02-29 2018-01-30 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Многоцелевая трансформируемая орбитальная система и способ ее применения
US10427804B1 (en) * 2016-04-29 2019-10-01 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US11267588B2 (en) * 2016-04-29 2022-03-08 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US10053241B2 (en) 2016-12-01 2018-08-21 The Boeing Company Systems and methods for multi-spacecraft distributed ascent
CN109539903B (zh) * 2018-10-31 2020-10-16 湖北航天技术研究院总体设计所 一种固体运载火箭椭圆转移轨道迭代制导控制方法
US20220185505A1 (en) * 2019-04-24 2022-06-16 Mitsubishi Electric Corporation Satellite constellation, ground facility and artificial satellite
CN110104219B (zh) * 2019-04-24 2020-09-08 中国人民解放军63920部队 一种控制探测器着陆地外天体的方法及装置
CN110543676B (zh) * 2019-07-31 2023-01-24 中南大学 一种基于代理模型的卫星集群构形重构规划方法及系统
KR102464559B1 (ko) * 2021-04-14 2022-11-09 한국항공우주연구원 궤도 천이 장치
CN114313313B (zh) * 2021-12-09 2023-02-28 哈尔滨工业大学 全电推进小卫星初始布轨至圆轨道的方法、装置及介质

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3907225A (en) * 1973-12-17 1975-09-23 Tru Inc Spacecraft for deploying objects into selected flight paths
US4504031A (en) * 1979-11-01 1985-03-12 The Boeing Company Aerodynamic braking and recovery method for a space vehicle
US5199672A (en) * 1990-05-25 1993-04-06 Orbital Sciences Corporation Method and apparatus for deploying a satellite network
US5393017A (en) * 1993-01-25 1995-02-28 Lockheed Missiles & Space Company, Inc. Technique for dispensing earth satellites into multi-planar orbits

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5681011A (en) * 1993-08-24 1997-10-28 Orbital Sciences Corporation Method for injecting payloads into orbit
US5595360A (en) * 1994-03-25 1997-01-21 Hughes Aircraft Company Optimal transfer orbit trajectory using electric propulsion

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3907225A (en) * 1973-12-17 1975-09-23 Tru Inc Spacecraft for deploying objects into selected flight paths
US4504031A (en) * 1979-11-01 1985-03-12 The Boeing Company Aerodynamic braking and recovery method for a space vehicle
US5199672A (en) * 1990-05-25 1993-04-06 Orbital Sciences Corporation Method and apparatus for deploying a satellite network
US5393017A (en) * 1993-01-25 1995-02-28 Lockheed Missiles & Space Company, Inc. Technique for dispensing earth satellites into multi-planar orbits

Also Published As

Publication number Publication date
EP0854083B1 (de) 2004-08-04
FR2757825A1 (fr) 1998-07-03
CN1195630A (zh) 1998-10-14
RU2220886C2 (ru) 2004-01-10
DE69730110T2 (de) 2004-12-09
FR2757825B1 (fr) 1999-03-26
DE69730110D1 (de) 2004-09-09
JPH1179100A (ja) 1999-03-23
US5961077A (en) 1999-10-05
EP0854083A1 (de) 1998-07-22

Similar Documents

Publication Publication Date Title
CN1083787C (zh) 使用高度偏心轨道和大气制动方法发射卫星的方法
CN1085168C (zh) 利用来自月球的引力帮助将卫星发射到不共面轨道上去的系统和方法
US5582367A (en) Elliptical orbit satellite, system, and deployment with controllable coverage characteristics
CN1083786C (zh) 利用高比冲量推进器将航天器送入轨道的方法和系统
US5788187A (en) Elliptical orbit satellite, system, and deployment with controllable coverage characteristics
US4759517A (en) Station-keeping using solar sailing
US7113851B1 (en) Practical orbit raising system and method for geosynchronous satellites
RU97121993A (ru) Способ и система одновременного выведения нескольких спутников на не являющиеся копланарными орбиты с использованием сильно эксцентрических орбит и атмосферного торможения
RU97121988A (ru) Способ и система выведения нескольких спутников на некопланарные орбиты с использованием силы лунного притяжения
CN1174982A (zh) 用于轨道偏航控制的动态偏置
EP2896570A1 (de) Verfahren und Vorrichtung zur Steuerung einer Vielzahl von Satelliten mit knotensynchroner Exzentrizitätssteuerung
Sergeyevsky et al. Interplanetary mission design handbook. Volume 1, part 2: Earth to Mars ballistic mission opportunities, 1990-2005
CN109911249A (zh) 低推重比飞行器的星际转移有限推力入轨迭代制导方法
US6042058A (en) Stationkeeping and momentum-dumping thruster systems and methods
CN111268177B (zh) 一种静止轨道卫星分散式闭环自主位置保持控制方法
McAdams et al. Trajectory design and maneuver strategy for the MESSENGER mission to Mercury
US7198230B2 (en) Method and system for maximizing satellite constellation coverage
EP0825508A1 (de) Verfahren zur Kopositionierung von Satelliten
Janson The on-orbit role of electric propulsion
Guo et al. New Horizons mission design for the Pluto-Kuiper Belt mission
EP0047211B1 (de) Verfahren zum Verändern der Umlaufbahn eines Satelliten, insbesondere zur Injektion in eine geostationäre Umlaufbahn, und für dieses Verfahren geeigneter Satellit
US3294344A (en) Changing the orientation and velocity of a spinning body traversing a path
BIRCH Orbital ring systems and Jacob's Ladders. III
CN117208231B (zh) 基于卫星推进剂约束的geo卫星最低入轨高度计算方法
KR20220094733A (ko) 달 플라이바이를 이용한 인공위성의 정지궤도 진입 방법 및 이를 이용한 소형 우주탐사선 사출 방법

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee